CAT III - longitudinal autolanding LQR design

Detalhes bibliográficos
Autor(a) principal: Marcos Vinícius Campos
Data de Publicação: 2006
Tipo de documento: Dissertação
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2910
Resumo: Automatic landings have been performed routinely for many years. However the design of flare and landing control systems with a suitable performance and a high level of reliability remains a very difficult task. In the present scenario, the increasing in the landing capacity of airports is mandatory by limiting the time each aircraft occupies the runway. To limit the occupancy time, the reduction of touchdown zone is essential since landings too close of the exit could result in a missed exit and therefore in a decreasing of landing rate. Give this context, the present work aims to propose an autoland flare law development for a 50 seat regional jet using Linear Quadratic Regulator technique. An accurate flare path, good rejection to turbulence, simplicity in implementation and, moreover, improved longitudinal touchdown dispersion are some of desirable features of design. In development of autoland control system, full feedback was used as control law configuration. Simulations were performed with non-linear model of the aircraft based on the equations of rigid body movement. The gains of LQR flare law were obtained though global optimization using Genetic Algorithms. The robustness of resulting close-loop system was tested with respect to ground-effect, wind shear and out-of-trim conditions. The performance of LQR flare law was compared with Model-Following design. Steady wind and turbulence models were used as disturbances for stochastic evaluation of the methods. The explicit flare trajectory defined in space, not in time, resulted on the improved touch down dispersion achieved by LQR design.
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spelling CAT III - longitudinal autolanding LQR designControle automático de aterrissagemRegulador linear quadráticoControle de vooControle longitudinalEstabilidade de aeronavesAerodinâmicaEngenharia aeronáuticaAutomatic landings have been performed routinely for many years. However the design of flare and landing control systems with a suitable performance and a high level of reliability remains a very difficult task. In the present scenario, the increasing in the landing capacity of airports is mandatory by limiting the time each aircraft occupies the runway. To limit the occupancy time, the reduction of touchdown zone is essential since landings too close of the exit could result in a missed exit and therefore in a decreasing of landing rate. Give this context, the present work aims to propose an autoland flare law development for a 50 seat regional jet using Linear Quadratic Regulator technique. An accurate flare path, good rejection to turbulence, simplicity in implementation and, moreover, improved longitudinal touchdown dispersion are some of desirable features of design. In development of autoland control system, full feedback was used as control law configuration. Simulations were performed with non-linear model of the aircraft based on the equations of rigid body movement. The gains of LQR flare law were obtained though global optimization using Genetic Algorithms. The robustness of resulting close-loop system was tested with respect to ground-effect, wind shear and out-of-trim conditions. The performance of LQR flare law was compared with Model-Following design. Steady wind and turbulence models were used as disturbances for stochastic evaluation of the methods. The explicit flare trajectory defined in space, not in time, resulted on the improved touch down dispersion achieved by LQR design.Instituto Tecnológico de AeronáuticaPedro PaglioneÁlvaro Vitor Polati de SouzaMarcos Vinícius Campos2006-03-10info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2910reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:04:59Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2910http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:40:18.694Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv CAT III - longitudinal autolanding LQR design
title CAT III - longitudinal autolanding LQR design
spellingShingle CAT III - longitudinal autolanding LQR design
Marcos Vinícius Campos
Controle automático de aterrissagem
Regulador linear quadrático
Controle de voo
Controle longitudinal
Estabilidade de aeronaves
Aerodinâmica
Engenharia aeronáutica
title_short CAT III - longitudinal autolanding LQR design
title_full CAT III - longitudinal autolanding LQR design
title_fullStr CAT III - longitudinal autolanding LQR design
title_full_unstemmed CAT III - longitudinal autolanding LQR design
title_sort CAT III - longitudinal autolanding LQR design
author Marcos Vinícius Campos
author_facet Marcos Vinícius Campos
author_role author
dc.contributor.none.fl_str_mv Pedro Paglione
Álvaro Vitor Polati de Souza
dc.contributor.author.fl_str_mv Marcos Vinícius Campos
dc.subject.por.fl_str_mv Controle automático de aterrissagem
Regulador linear quadrático
Controle de voo
Controle longitudinal
Estabilidade de aeronaves
Aerodinâmica
Engenharia aeronáutica
topic Controle automático de aterrissagem
Regulador linear quadrático
Controle de voo
Controle longitudinal
Estabilidade de aeronaves
Aerodinâmica
Engenharia aeronáutica
dc.description.none.fl_txt_mv Automatic landings have been performed routinely for many years. However the design of flare and landing control systems with a suitable performance and a high level of reliability remains a very difficult task. In the present scenario, the increasing in the landing capacity of airports is mandatory by limiting the time each aircraft occupies the runway. To limit the occupancy time, the reduction of touchdown zone is essential since landings too close of the exit could result in a missed exit and therefore in a decreasing of landing rate. Give this context, the present work aims to propose an autoland flare law development for a 50 seat regional jet using Linear Quadratic Regulator technique. An accurate flare path, good rejection to turbulence, simplicity in implementation and, moreover, improved longitudinal touchdown dispersion are some of desirable features of design. In development of autoland control system, full feedback was used as control law configuration. Simulations were performed with non-linear model of the aircraft based on the equations of rigid body movement. The gains of LQR flare law were obtained though global optimization using Genetic Algorithms. The robustness of resulting close-loop system was tested with respect to ground-effect, wind shear and out-of-trim conditions. The performance of LQR flare law was compared with Model-Following design. Steady wind and turbulence models were used as disturbances for stochastic evaluation of the methods. The explicit flare trajectory defined in space, not in time, resulted on the improved touch down dispersion achieved by LQR design.
description Automatic landings have been performed routinely for many years. However the design of flare and landing control systems with a suitable performance and a high level of reliability remains a very difficult task. In the present scenario, the increasing in the landing capacity of airports is mandatory by limiting the time each aircraft occupies the runway. To limit the occupancy time, the reduction of touchdown zone is essential since landings too close of the exit could result in a missed exit and therefore in a decreasing of landing rate. Give this context, the present work aims to propose an autoland flare law development for a 50 seat regional jet using Linear Quadratic Regulator technique. An accurate flare path, good rejection to turbulence, simplicity in implementation and, moreover, improved longitudinal touchdown dispersion are some of desirable features of design. In development of autoland control system, full feedback was used as control law configuration. Simulations were performed with non-linear model of the aircraft based on the equations of rigid body movement. The gains of LQR flare law were obtained though global optimization using Genetic Algorithms. The robustness of resulting close-loop system was tested with respect to ground-effect, wind shear and out-of-trim conditions. The performance of LQR flare law was compared with Model-Following design. Steady wind and turbulence models were used as disturbances for stochastic evaluation of the methods. The explicit flare trajectory defined in space, not in time, resulted on the improved touch down dispersion achieved by LQR design.
publishDate 2006
dc.date.none.fl_str_mv 2006-03-10
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2910
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2910
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Controle automático de aterrissagem
Regulador linear quadrático
Controle de voo
Controle longitudinal
Estabilidade de aeronaves
Aerodinâmica
Engenharia aeronáutica
_version_ 1706809292232851456